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Boundary layer separation in internal flow

Author(s)
Moses, Hal Lynwood; Chappell, John R.; Goldberger, Tomas
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Other Contributors
David W. Taylor Model Basin
United States. Navy Department. Bureau of Ships. Fundamental Hydromechanics Research Program
Massachusetts Institute of Technology. Gas Turbine Laboratory
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Abstract
An investigation of incompressible turbulent boundary layer separation in internal flow is presented with experimental results for a variable geometry, two-dimensional diffuser and two conical diffusers. A simple analytical model is adopted, which consists of wall boundary layers and a one-dimensional, inviscid core. Several approximate boundary layer methods and the possibility of extending them into the separated region are examined. With a limited amount of separated flow, the calculated pressure agrees reasonably well with the experimental results and gives a fair indication of maximum diffuser performance. The limitations of the model to the more general problem, as well as the problem of singularities and downstream stability, are discussed.
Description
September 1965
 
Includes bibliographical references
 
Date issued
1965
URI
http://hdl.handle.net/1721.1/104679
Publisher
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1965]
Series/Report no.
GTL report #81

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